An improved progressive damage model for three-dimensional five-directional braided composites under longitudinal compression

被引:0
作者
Tang, Shaofeng [1 ]
Fu, Kunkun [1 ,2 ]
Li, Yan [1 ,2 ]
机构
[1] Tongji Univ, Sch Aerosp Engn & Appl Mech, Shanghai 200092, Peoples R China
[2] Tongji Univ, Shanghai Inst Aircraft Mech & Control, Shanghai 200092, Peoples R China
关键词
A. Polymer-matrix composites (PMCs); E; Braiding; B. Mechanical properties; C. Finite element analysis (FEA); FIBER-REINFORCED COMPOSITES; MECHANICAL-PROPERTIES; FAILURE CRITERIA; STRENGTH; EMPHASIS; BEHAVIOR; KINKING;
D O I
10.1016/j.compositesa.2025.108880
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Various failure modes of three-dimensional five-directional braided composites (3D5DBCs) under longitudinal compression have been observed, including yarn fracture and kinking, transverse inter-fiber cracking, matrix plastic deformation/fracture and fiber/matrix interfacial debonding, leading to the difficulty in predicting their mechanical properties. This study proposes an improved progressive damage model for 3D5DBCs under longitudinal compression, addressing all the observed failure modes. Then, the proposed progressive damage model is implemented in a finite element (FE) model to predict the mechanical responses and properties of 3D5DBCs under longitudinal compression. The numerical predictions in terms of compressive stress-strain relations, compressive strengths and failure modes are in good agreement with the experimental results, demonstrating the effectiveness of the proposed progressive damage model. Finally, the failure envelopes of 3D5DBCs under compression-shear loading are predicted using our FE model, and the effectiveness of several classical failure criteria on the strength prediction of 3D5DBCs is discussed.
引用
收藏
页数:12
相关论文
共 44 条
[1]  
Bazant ZP, 1983, Materiaux et construction, V16, P155, DOI [10.1007/BF02486267, DOI 10.1007/BF02486267]
[2]   Shear characterization of para-aramid (Twaron®) fabric by yarn pull-out method [J].
Bilisik, Kadir .
TEXTILE RESEARCH JOURNAL, 2012, 82 (14) :1442-1456
[3]   Mesomechanical Model for Numerical Study of Two-Dimensional Triaxially Braided Composite [J].
Binienda, Wieslaw K. ;
Li, Xuetao .
JOURNAL OF ENGINEERING MECHANICS, 2010, 136 (11) :1366-1379
[4]   Size-dependency of the transverse-tensile failure behavior for triaxially braided composites [J].
Cai, Yinglong ;
Zhao, Zhenqiang ;
Tie, Ying ;
Cao, Yong ;
Chen, Jiangyi ;
Binienda, Wieslaw K. ;
Zhang, Chao .
COMPOSITES SCIENCE AND TECHNOLOGY, 2021, 206
[5]  
[陈利 Chen Li], 2005, [材料工程, Journal of Materials Engineering], V0, P3
[6]   Failure and damage characterization of (±30°) biaxial braided composites under multiaxial stress states [J].
Cichosz, Joerg ;
Wehrkamp-Richter, Tobias ;
Koerber, Hannes ;
Hinterhoelz, Roland ;
Camanho, Pedro P. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2016, 90 :748-759
[7]   The predictive capability of failure mode concept-based strength criteria for multidirectional laminates [J].
Cuntze, RG ;
Freund, A .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (3-4) :343-377
[8]   Progressive damage and nonlinear analysis of 3D four-directional braided composites under unidirectional tension [J].
Fang Guo-dong ;
Liang Jun ;
Wang Bao-lai .
COMPOSITE STRUCTURES, 2009, 89 (01) :126-133
[9]   Investigation on the compressive properties of the three dimensional four-directional braided composites [J].
Fang, Guodong ;
Liang, Jun ;
Lu, Qi ;
Wang, Baolai ;
Wang, Yu .
COMPOSITE STRUCTURES, 2011, 93 (02) :392-405
[10]   Prediction of mechanical properties on 3D braided composites with void defects [J].
Gao, Xuhao ;
Yuan, Li ;
Fu, Yutong ;
Yao, Xuefeng ;
Yang, Heng .
COMPOSITES PART B-ENGINEERING, 2020, 197